JPH0760770A - Frp solid molding method - Google Patents
Frp solid molding methodInfo
- Publication number
- JPH0760770A JPH0760770A JP5210077A JP21007793A JPH0760770A JP H0760770 A JPH0760770 A JP H0760770A JP 5210077 A JP5210077 A JP 5210077A JP 21007793 A JP21007793 A JP 21007793A JP H0760770 A JPH0760770 A JP H0760770A
- Authority
- JP
- Japan
- Prior art keywords
- frp
- prepreg
- rubber sheet
- core material
- jig
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Landscapes
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明はFRP(繊維強化プラス
チック)の立体成形法に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a three-dimensional molding method of FRP (fiber reinforced plastic).
【0002】[0002]
【従来の技術】シート状のFRPプリプレグ(以下、プ
リプレグと略称)を積層して立体形状を得る従来からの
方法としては、手作業により一枚ずつ押さえつけて形状
になじませる方法の他、作業効率のよい方法として図5
に示す方法がある。この方法はツール面3上の必要な形
状のコア材5の上にプリプレグ2を必要枚数載せて、最
終的にラバーシート1を被せて周囲を密封し、真空引き
4によるラバーシート1の密着を利用して必要形状を得
る方法である。2. Description of the Related Art Conventional methods for stacking sheet-like FRP prepregs (hereinafter abbreviated as prepregs) to obtain a three-dimensional shape include a method of manually pressing one by one to adjust the shape, and work efficiency. Figure 5
There is a method shown in. In this method, a required number of prepregs 2 are placed on a core material 5 having a required shape on the tool surface 3, and finally a rubber sheet 1 is covered to seal the periphery, and the rubber sheet 1 is adhered by vacuuming 4. This is a method for obtaining the required shape.
【0003】[0003]
【発明が解決しようとする課題】図5で説明した従来方
法は図6に示すように、形状によってはプリプレグ2の
端部(A部)が真空引き孔4からの真空引きによりツー
ル面3に先に押さえつけられて動かなくなり、プリプレ
グ2全体がコア材5のB部へ密着することが防げられ、
コア材5の形状に応じた形状が得られなかったり、欠陥
の入った製品となる場合がある。従って、真空引きを利
用した方法は適用範囲がかなり限られていた。According to the conventional method described with reference to FIG. 5, as shown in FIG. 6, the end portion (A portion) of the prepreg 2 is moved to the tool surface 3 by vacuum drawing from the vacuum drawing hole 4 depending on the shape. It is pressed down first and becomes immovable, and it is possible to prevent the entire prepreg 2 from sticking to part B of the core material 5,
In some cases, the shape corresponding to the shape of the core material 5 may not be obtained, or the product may have defects. Therefore, the method utilizing vacuum evacuation has a fairly limited application range.
【0004】本発明は上記技術水準に鑑み、従来法にお
けるような不具合が発生しないFRPの立体成形法を提
供しようとするものである。In view of the above-mentioned state of the art, the present invention is to provide a three-dimensional molding method of FRP which does not cause the problems as in the conventional method.
【0005】[0005]
【課題を解決するための手段】本発明は (1)ツール面上に希望する形状のコア材を設置し、該
コア材を覆うように順次FRPプリプレグ及びラバーシ
ートを配設し、該ラバーシート内を真空引きすることに
よって前記コア材に前記FRPプリプレグを密着させて
コア材に合致する形状のFRP立体成形物を得る方法に
おいて、前記FRPプリプレグの端部と前記ラバーシー
トの端部の間に、一定高さの治具を配設して真空引きを
することを特徴とするFRP立体成形法。 (2)一定高さの治具の代わりに、バネ、伸縮性材料ま
たは可倒式器具よりなる高さの変わる治具を用いたこと
を特徴とする上記(1)記載のFRP立体成形法。 (3)真空引きと同時に加熱を付与することを特徴とす
る上記(1)または(2)に記載のFRP立体成形法。
である。According to the present invention, (1) a core material having a desired shape is installed on a tool surface, an FRP prepreg and a rubber sheet are sequentially arranged so as to cover the core material, and the rubber sheet is provided. A method for obtaining an FRP three-dimensional molded article having a shape conforming to the core material by bringing the FRP prepreg into close contact with the core material by vacuuming the inside, and between the end portion of the FRP prepreg and the end portion of the rubber sheet. The FRP three-dimensional molding method is characterized in that a jig having a constant height is arranged and a vacuum is drawn. (2) The FRP three-dimensional molding method according to the above (1), wherein a jig having a variable height, which is made of a spring, a stretchable material or a retractable device, is used instead of the jig having a constant height. (3) The FRP three-dimensional molding method according to the above (1) or (2), characterized in that heating is applied simultaneously with evacuation.
Is.
【0006】すなわち、本発明はラバーシートの内側に
治具を配置して、最初ラバーシートが浮いた状態で真空
引きを開始することによりプリプレグの端部がツール面
に密着する時期を遅らせてプリプレグがコア材に完全に
密着して所望の成形体になるようにするものである。That is, according to the present invention, a jig is arranged inside a rubber sheet, and vacuuming is started in a state where the rubber sheet is first floated, thereby delaying the time when the end of the prepreg comes into close contact with the tool surface. Completely adheres to the core material to form a desired molded body.
【0007】本発明で使用される治具は一定高さの金属
などの剛性のものが一般的であるが、高さが変化する治
具、例えばバネ、伸縮性材料よりなる治具、可倒式器具
などを用いることもできる。The jig used in the present invention is generally made of a rigid material such as metal having a fixed height, but a jig whose height changes, for example, a spring, a jig made of a stretchable material, A formula tool or the like can also be used.
【0008】真空引きのみによると、プリプレグの動き
が悪い場合には、上記治具と併用して加熱を行なうこと
が好ましい。加熱はプリプレグの硬化があまり進行しな
い温度・時間の範囲内で樹脂粘度が適度に低くなる温度
を設定する。プリプレグの硬化はプリプレグの成形後に
引き続き硬化温度まで加熱するか、オートクレーブ等の
装置に置き直して加熱、硬化させる。According to only evacuation, when the movement of the prepreg is bad, it is preferable to perform heating in combination with the above jig. The heating is set to a temperature at which the resin viscosity is appropriately lowered within a temperature / time range where curing of the prepreg does not proceed so much. The prepreg is cured by heating it to the curing temperature after molding the prepreg or placing it in an apparatus such as an autoclave to heat and cure it.
【0009】本発明はカーボン繊維、アラミド繊維、ガ
ラス繊維などで強化されたエポキシ樹脂、フェノール樹
脂などの熱硬化性樹脂よりなるFRPの立体成形に有利
に採用し得る。The present invention can be advantageously applied to the three-dimensional molding of FRP made of a thermosetting resin such as epoxy resin or phenol resin reinforced with carbon fiber, aramid fiber, glass fiber or the like.
【0010】[0010]
【作用】ラバーシート内を真空引きしてゆくと、大気圧
によりラバーシートの外側から加圧されて、プリプレグ
は先ずコア材の凸部に密着する。ラバーシートの周囲が
低ければラバーシートの周囲部もツール面に密着し、続
いてプリプレグもツール面に密着してコア材に密着する
ことが妨げられるが、ラバーシートの周囲を治具によっ
て持ち上げ、ラバーシートのツール面への密着する時期
を遅らせることによって、プリプレグがコア材の形状に
なじむように密着するまでプリプレグの端部がツール面
に密着するのが防がれる。When the inside of the rubber sheet is evacuated, the prepreg is first brought into close contact with the convex portion of the core material by being pressurized from the outside of the rubber sheet by the atmospheric pressure. If the circumference of the rubber sheet is low, the periphery of the rubber sheet will also adhere to the tool surface, and then the prepreg will also adhere to the tool surface, preventing it from adhering to the core material. By delaying the time when the rubber sheet adheres to the tool surface, it is possible to prevent the end of the prepreg from adhering to the tool surface until the prepreg conforms to the shape of the core material.
【0011】さらに加熱を併用した場合には、樹脂粘度
の低下により、ツール面とプリプレグのすべりがよくな
り、またプリプレグ自体もやわらかくなるため、コア材
の形状になじみ易くなる。Further, when heating is also used, the viscosity of the resin is lowered, the sliding of the prepreg on the tool surface is improved, and the prepreg itself becomes soft, so that the shape of the core material is easily adapted.
【0012】[0012]
【実施例】以下、航空機等の複合材製補強外板に必要な
ストリンガでハット型ストリンガを成形する場合の実施
例を示す。EXAMPLE An example of forming a hat type stringer with a stringer required for a composite reinforced outer plate of an aircraft will be described below.
【0013】(実施例1)この実施例を図1によって説
明する。図1において、1はシリコンラバーシート、2
はカーボン繊維で強化されたエポキシ樹脂よりなるFR
Pのプリプレグ、3はツール面、4は真空引き孔、5は
台形断面で底角が45°、高さ18mmのコア材、6は
直方形断面で高さ18mmの金属製治具を示す。図1に
示すように、各部材をツール面3上に配置し、真空引き
孔4より真空引きして、シリコンラバーシート内の圧力
を−650mmHgにし、かつ50℃に加熱して実施し
たところ、プリプレグ2はコア材5の側面に相当する部
分にも隙間がなく密着させることができた。(Embodiment 1) This embodiment will be described with reference to FIG. In FIG. 1, 1 is a silicone rubber sheet, 2
Is an FR made of epoxy resin reinforced with carbon fiber
A prepreg of P, 3 is a tool surface, 4 is a vacuum hole, 5 is a core material having a trapezoidal cross section with a base angle of 45 ° and a height of 18 mm, and 6 is a metal jig having a rectangular cross section with a height of 18 mm. As shown in FIG. 1, each member was placed on the tool surface 3, vacuumed through the vacuum holes 4, the pressure inside the silicone rubber sheet was -650 mmHg, and heating to 50 ° C. was performed. The prepreg 2 could be adhered to the part corresponding to the side surface of the core material 5 without any gap.
【0014】(実施例2)上記実施例1の治具6に代わ
りに、図2に示すようにバネ7を使用し、真空引き前は
シリコンラバーシート1を浮かせた状態にしておき、真
空引き後は該シリコンラバーシート1をツール面3の近
くまで低くなるようにして、実施例1と同様に実施した
ところ、実施例1と同様の結果が得られた。さらに、こ
の実施例のバネ7の代わりに、図3に示すような伸縮性
治具(スポンジ状のものなど)8、図4に示すような可
倒式治具9を使用し、同様に実施しても同様な結果が得
られた。(Embodiment 2) Instead of the jig 6 of the above Embodiment 1, a spring 7 is used as shown in FIG. 2, and the silicon rubber sheet 1 is left in a floating state before evacuation, and evacuation is performed. After that, when the silicone rubber sheet 1 was lowered to the vicinity of the tool surface 3 and the same procedure as in Example 1 was performed, the same results as in Example 1 were obtained. Further, instead of the spring 7 of this embodiment, a stretchable jig (sponge-like one) 8 as shown in FIG. 3 and a retractable jig 9 as shown in FIG. Even if the same result was obtained.
【0015】[0015]
【発明の効果】本発明によれば、ラバーシートがツール
面に密着するタイミングをコントロールすることによ
り、従来、プリプレグ端部がツール面に押さえられて立
体形状化が難しかった場合についても、真空を利用した
立体形状化方法が適用でき、成形作業の簡易化、コスト
低減の効果が得られる。According to the present invention, by controlling the timing at which the rubber sheet comes into close contact with the tool surface, the vacuum can be maintained even when it has been difficult to form a three-dimensional shape by pressing the prepreg end portion against the tool surface. The three-dimensional shaping method used can be applied, and the effects of simplifying the molding work and reducing the cost can be obtained.
【図1】本発明の一定高さの治具を用いた実施例の説明
図。FIG. 1 is an explanatory diagram of an embodiment using a jig having a constant height according to the present invention.
【図2】本発明のバネを治具として用いた実施例の説明
図。FIG. 2 is an explanatory view of an embodiment using the spring of the present invention as a jig.
【図3】本発明の伸縮性材料を治具として用いた実施例
の説明図。FIG. 3 is an explanatory diagram of an example in which the stretchable material of the present invention is used as a jig.
【図4】本発明の可倒式器具を治具として用いた実施例
の説明図。FIG. 4 is an explanatory diagram of an embodiment in which the folding instrument of the present invention is used as a jig.
【図5】従来の真空を利用するプリプレグの立体成形の
一態様の説明図。FIG. 5 is an explanatory view of one aspect of conventional three-dimensional molding of a prepreg using vacuum.
【図6】従来法の問題点を示す説明図。FIG. 6 is an explanatory diagram showing the problems of the conventional method.
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 B29L 9:00 ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification code Internal reference number FI technical display location B29L 9:00
Claims (3)
置し、該コア材を覆うように順次FRPプリプレグ及び
ラバーシートを配設し、該ラバーシート内を真空引きす
ることによって前記コア材に前記FRPプリプレグを密
着させてコア材に合致する形状のFRP立体成形物を得
る方法において、前記FRPプリプレグの端部と前記ラ
バーシートの端部の間に、一定高さの治具を配設して真
空引きをすることを特徴とするFRP立体成形法。1. A core material having a desired shape is installed on a tool surface, an FRP prepreg and a rubber sheet are sequentially arranged so as to cover the core material, and the inside of the rubber sheet is evacuated to vacuum the core material. In the method for obtaining an FRP three-dimensional molded article having a shape conforming to the core material by closely contacting the FRP prepreg with the above, a jig having a constant height is provided between the end of the FRP prepreg and the end of the rubber sheet. The FRP solid molding method is characterized by performing vacuuming.
性材料または可倒式器具よりなる高さの変わる治具を用
いたことを特徴とする請求項1記載のFRP立体成形
法。2. The FRP three-dimensional molding method according to claim 1, wherein a jig having a variable height, which is made of a spring, a stretchable material, or a retractable device, is used instead of the jig having a constant height. .
特徴とする請求項1または2に記載のFRP立体成形
法。3. The FRP three-dimensional molding method according to claim 1, wherein heating is applied simultaneously with the evacuation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5210077A JPH0760770A (en) | 1993-08-25 | 1993-08-25 | Frp solid molding method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5210077A JPH0760770A (en) | 1993-08-25 | 1993-08-25 | Frp solid molding method |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0760770A true JPH0760770A (en) | 1995-03-07 |
Family
ID=16583440
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP5210077A Withdrawn JPH0760770A (en) | 1993-08-25 | 1993-08-25 | Frp solid molding method |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0760770A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002172630A (en) * | 2000-12-06 | 2002-06-18 | Toray Ind Inc | Vacuum-molding method for frp |
WO2010079865A1 (en) * | 2009-01-08 | 2010-07-15 | 주식회사 대한항공 | Prepreg folding and forming apparatus and forming method thereof |
WO2012133534A1 (en) | 2011-03-31 | 2012-10-04 | 三菱重工業株式会社 | Molding method and molding device for composite material hollow part |
JP2016088090A (en) * | 2014-10-29 | 2016-05-23 | ザ・ボーイング・カンパニーThe Boeing Company | Method, device and apparatus for vacuum-forming composite laminates |
CN105965915A (en) * | 2015-03-11 | 2016-09-28 | 富士重工业株式会社 | Device for molding of composite material and method therefor |
-
1993
- 1993-08-25 JP JP5210077A patent/JPH0760770A/en not_active Withdrawn
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002172630A (en) * | 2000-12-06 | 2002-06-18 | Toray Ind Inc | Vacuum-molding method for frp |
WO2010079865A1 (en) * | 2009-01-08 | 2010-07-15 | 주식회사 대한항공 | Prepreg folding and forming apparatus and forming method thereof |
WO2012133534A1 (en) | 2011-03-31 | 2012-10-04 | 三菱重工業株式会社 | Molding method and molding device for composite material hollow part |
US9403302B2 (en) | 2011-03-31 | 2016-08-02 | Mitsubishi Heavy Industries, Ltd. | Fabrication method and fabrication device for composite material hollow part |
JP2016088090A (en) * | 2014-10-29 | 2016-05-23 | ザ・ボーイング・カンパニーThe Boeing Company | Method, device and apparatus for vacuum-forming composite laminates |
CN105965915A (en) * | 2015-03-11 | 2016-09-28 | 富士重工业株式会社 | Device for molding of composite material and method therefor |
US10328615B2 (en) | 2015-03-11 | 2019-06-25 | Subaru Corporation | Molding equipment of composite material and molding method of composite material |
CN105965915B (en) * | 2015-03-11 | 2021-06-18 | 株式会社斯巴鲁 | Apparatus and method for molding composite material |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 20001031 |